Two satellite are revolving around the earth with velocities v₁ and  v₂ and in radii  r₁ and r₂(r₁ > r₂) respectively. Then

• A

  ${\mathrm{v}}_1={\mathrm{v}}_2$

• B

  ${\mathrm{v}}_1>{\mathrm{v}}_2$

• C

  ${\mathrm{v}}_1<{\mathrm{v}}_2$

• D

  $\frac{{\mathrm{v}}_1}{{\mathrm{r}}_1}=\frac{{\mathrm{v}}_2}{{\mathrm{r}}_2}$